Device for emulating temperature of a composite structure through a thermal cure cycle
A temperature emulator may include a stack assembly having a pair of end plates positioned at an uppermost and lowermost location of the stack assembly, a plurality of heat sink plates disposed between the pair of end plates, each of the heat sink plates having a plurality of heat sink cutouts, a plurality of shim plates separating adjacent pairs of the end plates and the heat sink plates, each of the shim plates having a shim cutout, an open cavity formed by a plurality of adjacent heat sink cutouts and shim cutouts, thermal insulation disposed within the cavity, and at least one temperature sensor coupled to at least one of the plurality of heat sink plates.
1. A method of emulating a thermal inertia gradient of a composite part, said method comprising:
providing a pair of end plates, a plurality of heat sink plates each comprising a plurality of heat sink cutouts, and a plurality of shim plates each comprising a shim cutout;
stack assembling said plurality of heat sink plates, wherein adjacent pairs of heat sink plates are separated by at least one of said plurality of shim plates such that a plurality of adjacent heat sink cutouts and shim cutouts form a cavity;
assembling said pair of end plates to form a stack assembly;
applying thermal insulation within said cavity;
creating a thermal model of said stack assembly; and
identifying a thermal profile of said stack assembly.
2. The method of claim 1 further comprising:
identifying a thermal profile of said composite part; and
comparing said thermal profile of said stack assembly to said thermal profile of said composite part.
3. The method of claim 2 further comprising:
determining a configuration of said stack assembly having a thermal profile matching said thermal profile of said composite part; and
adding shim plates to or subtracting shim plates from said stack assembly based on said configuration.
4. The method of claim 2 further comprising:
determining a configuration of said stack assembly having a thermal profile matching said thermal profile of said composite part; and
adding heat sink plates to or subtracting heat sink plates from said stack assembly based on said configuration.
5. The method of claim 2 further comprising:
determining a configuration of said stack assembly having a thermal profile matching said thermal profile of said composite part;
adding shim plates to or subtracting shim plates from said stack assembly based on said configuration; and
adding heat sink plates to or subtracting heat sink plates from said stack assembly based on said configuration.
6. The method of claim 1 further comprising:
coupling at least one temperature sensor to at least one of said heat sink plates;
positioning said stack assembly with at least one temperature sensor in an autoclave in proximity to at least one composite part having a matching thermal profile; and,
monitoring a thermal inertia gradient of said stack assembly.
7. The method of claim 1 further comprising coupling at least one temperature sensor to at least one of said heat sink plates.
8. The method of claim 7 further comprising positioning said stack assembly with at least one temperature sensor in an autoclave in proximity to at least one composite part having a matching thermal profile.
9. The method of claim 8 further comprising monitoring a thermal inertia gradient of said stack assembly.
10. The method of claim 9 further comprising the step of adjusting control settings of an autoclave in response to said thermal inertia gradient of said stack assembly throughout a thermal cure cycle.
11. The method of claim 7 wherein each heat sink plate of said plurality of heat sink plates further comprises a center portion.
12. The method of claim 11 wherein said temperature sensor is coupled to said center portion.
13. The method of claim 11 wherein each heat sink plate of said plurality of heat sink plates comprises a channel extending from a perimeter edge to proximate a center of said center portion to receive said temperature sensor.
14. The method of claim 7 wherein said temperature sensor comprises a thermocouple.
15. The method of claim 1 wherein said thermal insulation comprises a powder.
16. The method of claim 1 wherein said thermal insulation comprises silica aerogel powder.
17. The method of claim 1 wherein said plurality of heat sink cutouts comprises a plurality of generally arcuate outer cutouts and a plurality of generally arcuate inner cutouts spaced apart from said outer cutouts.
18. The method of claim 1 further comprising securing together said stack assembly using a plurality of fasteners.
19. The method of claim 1 wherein a first shim plate of said plurality of shim plates has a first thickness and a second shim plate of said plurality of shim plates has a second thickness, said first thickness being different from said second thickness.
20. The method of claim 1 wherein each shim plate of said plurality of shim plates has a thickness ranging from about 0.010 inch to about 0.125 inch.